Analysis on Circumferential Seal Ring in Engine under Different Conditions

Article Preview

Abstract:

Utilizing ANSYS to analyze the performance of the circumferential seal ring under the condition of different temperatures and different rotational speeds and get the rings value of the maximum stress, the maximum strain, the maximum contact pressure on main sealing surface respectively. By analyzing the change of these values to reveal the change rule of the seal ring, thus provide the basis for designing and selecting the circumferential seal ring.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 945-949)

Pages:

343-346

Citation:

Online since:

June 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Bruce M. Steinefz, Robert C. Hendricks. Advanced Seal Technology in Meeting Next Generation Turbine Engine Goal[R]. NASA/TM-1998-206961.

Google Scholar

[2] Wei Wang, Zongjian Zhao, Zhensheng Zhang: Aeroengine. 2009, 35(4), 11-15. (in Chinese).

Google Scholar

[3] Chunxin Chen, Bo Qiu, Jun Li, et al: Journal of XI an Jiaotong University. 2011, 45(5), 36-41. (in Chinese).

Google Scholar

[4] Quanbin Ren, Ruxun Chen, Weiguo Yang: Journal of Aerospace Power. 1995, 10(3), 241-310. (in Chinese).

Google Scholar

[5] Lisheng Zheng: Thermal Structural Analysis of Circumferential Seal in Aeroengines [D]. Shenyang: Northeastern University. 2013. (in Chinese).

Google Scholar

[6] Jian Li, ZhiQuan Liu. Journal of Aerospace Power. 1999, 14(3), 242-246. (in Chinese).

Google Scholar

[7] Xiaoliang Shan, Yuli Hu. Lubrication Engineering. 2006, 9, 116-119. (in Chinese).

Google Scholar

[8] Youhong Liu, Chao Yu: Science Technology and Engineering. 2009, 9(22), 6922-6925. ( in Chinese).

Google Scholar